首页> 外国专利> AUTOMATIC GUIDANCE SYSTEM FOR FLIGHT VEHICLE HAVING PARAFOIL AND NAVIGATION GUIDANCE APPARATUS FOR THE SYSTEM

AUTOMATIC GUIDANCE SYSTEM FOR FLIGHT VEHICLE HAVING PARAFOIL AND NAVIGATION GUIDANCE APPARATUS FOR THE SYSTEM

机译:具有翼型的飞行器自动制导系统和该系统的导航制导装置

摘要

An automatic guidance system guides a flight vehicle having a parafoil to a target grounding point. The system opens the parafoil of the flight vehicle dropped in a predetermined area above the target grounding point. The system estimates wind velocity and wind direction after the parafoil of the flight vehicle is opened. Then, the system determines the landing flight path of the flight vehicle based on the estimated wind velocity and wind direction, guides the flight of the flight vehicle to the determined landing flight path and descends the flight vehicle according to the landing flight path.
机译:自动引导系统将具有翼型的飞行器引导至目标接地点。该系统打开落在目标接地点上方预定区域的飞行器的机翼。在飞行器的翼型打开之后,系统估计风速和风向。然后,系统基于估计的风速和风向确定飞行器的着陆飞行路径,将飞行器的飞行引导至确定的着陆飞行路径,并根据着陆飞行路径使飞行器下降。

著录项

  • 公开/公告号CA2290118C

    专利类型

  • 公开/公告日2007-07-10

    原文格式PDF

  • 申请/专利权人 FUJI JUKOGYO KABUSHIKI KAISHA;

    申请/专利号CA19992290118

  • 发明设计人 YONEDA HIROSHI;AMITO ATSUSHI;

    申请日1999-11-22

  • 分类号G05D1/12;G05D1/10;

  • 国家 CA

  • 入库时间 2022-08-21 20:54:11

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